BE519699A - - Google Patents
Info
- Publication number
- BE519699A BE519699A BE519699DA BE519699A BE 519699 A BE519699 A BE 519699A BE 519699D A BE519699D A BE 519699DA BE 519699 A BE519699 A BE 519699A
- Authority
- BE
- Belgium
- Prior art keywords
- wheels
- compressor
- rotating
- turbine
- wheel
- Prior art date
Links
- 238000007906 compression Methods 0.000 claims description 4
- 230000001808 coupling Effects 0.000 claims description 3
- 239000012530 fluid Substances 0.000 claims description 3
- 210000001503 Joints Anatomy 0.000 claims description 2
- 238000001764 infiltration Methods 0.000 claims 1
- 238000003466 welding Methods 0.000 claims 1
- 239000003921 oil Substances 0.000 description 11
- 230000001050 lubricating Effects 0.000 description 5
- 230000036633 rest Effects 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 3
- 239000007789 gas Substances 0.000 description 2
- YSSSPARMOAYJTE-UHFFFAOYSA-N Dibenzo-18-crown-6 Chemical class O1CCOCCOC2=CC=CC=C2OCCOCCOC2=CC=CC=C21 YSSSPARMOAYJTE-UHFFFAOYSA-N 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000000875 corresponding Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000002093 peripheral Effects 0.000 description 1
- 239000003638 reducing agent Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000000284 resting Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Publications (1)
Publication Number | Publication Date |
---|---|
BE519699A true BE519699A (de) |
Family
ID=155834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BE519699D BE519699A (de) |
Country Status (1)
Country | Link |
---|---|
BE (1) | BE519699A (de) |
-
0
- BE BE519699D patent/BE519699A/fr unknown
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3071792B1 (de) | Modulares triebwerk | |
CA2635632C (fr) | Turbomachine a double soufflante | |
EP2834475B1 (de) | Kraftübertragungssystem für eine turbomaschine und entsprechendes verfahren | |
EP2396525B1 (de) | System von kompakten gegenläufigen propellern | |
EP3137741B1 (de) | Flugzeugtriebwerk mit verbessertem der ziehen mechanischen leistung | |
FR2950381A1 (fr) | Turbomachine a helices non carenees contrarotatives | |
WO2015189522A1 (fr) | Turbomachine comprenant un systeme d'entrainement d'un equipement tel qu'un boitier d'accessoires | |
FR3130875A1 (fr) | Module de turbomachine equipe d’aubes a calage variable et d’un dispostif de transfert d’huile | |
CA2947249A1 (fr) | Assemblage pour turbomachine d'aeronef et son procede de montage | |
FR3043714A1 (fr) | Partie avant de turbomachine d'aeronef comprenant une soufflante unique entrainee par un reducteur, ainsi que des aubes directrices de sortie structurales agencees en partie en amont d'un bec de separation | |
FR2987402A1 (fr) | Dispositif de lubrification d'un reducteur epicycloidal compatible d'un montage modulaire. | |
FR3087223A1 (fr) | Turbomachine a turbine contrarotative pour un aeronef | |
EP3673164B1 (de) | Zweiwellen-mantelstrom-triebwerk mit einem niederdruckwellenschublager im abgasgehäuse | |
FR2856440A1 (fr) | Compresseur de turbomachine et roue dudit compresseur | |
FR3027625A1 (fr) | Turbomachine comprenant un generateur de courant electrique permettant l'injection d'huile depuis l'interieur d'un arbre de turbine | |
EP3861195A1 (de) | Turbofantriebwerk mit einem durch seine sekundärströmung gekühlten auslasskegel | |
EP4150199A1 (de) | Turbomaschine eines luftfahrzeugs, die eine schmiervorrichtung eines lagers umfasst | |
EP4073354B1 (de) | Unterdrucksetzung von schmierkammern in einer turbomaschine mit gegenläufiger turbine | |
BE519699A (de) | ||
BE1025131A1 (fr) | Arbre de transmission à double cannelure pour turbomachine | |
EP1473462B1 (de) | Patrone zum Zusammenbau eines Verdichters | |
FR3118483A1 (fr) | Module de turbomachine equipe d’une machine electrique et turbomachine equipee d’un tel module | |
WO2020183074A2 (fr) | Turbine à gaz pour aéronef à double rotor | |
FR3039212A1 (fr) | Sous-ensemble de turbomachine comportant un accessoire entraine par une roue montee sur des pales de rotor | |
BE468781A (de) |